EP 3332108 B1 20190529 - METHOD FOR CONTROLLING THE PRESSURE AND A MIXTURE RATIO OF A ROCKET ENGINE, AND CORRESPONDING DEVICE
Title (en)
METHOD FOR CONTROLLING THE PRESSURE AND A MIXTURE RATIO OF A ROCKET ENGINE, AND CORRESPONDING DEVICE
Title (de)
VERFAHREN ZUR STEUERUNG DES DRUCKS UND EINES MISCHUNGSVERHÄLTNISSES EINES RAKETENTRIEBWERKS UND ENTSPRECHENDE VORRICHTUNG
Title (fr)
PROCÉDÉ DE CONTRÔLE DE LA PRESSION ET D'UN RAPPORT DE MÉLANGE D'UN MOTEUR DE FUSÉE, ET DISPOSITIF CORRESPONDANT
Publication
Application
Priority
- FR 1501683 A 20150806
- FR 2016052011 W 20160802
Abstract (en)
[origin: WO2017021651A1] The invention relates to a method and device for controlling the pressure (PGC) and a mixture ratio of a rocket engine on the basis of a set pressure value (PGCc) and set mixture ratio value (RMc). In said method and device, a control generates signals for controlling two control valves (VR1, VR2) of said engine, the control using a pressure feedback loop. Said control also uses a determination of an estimated mixture ratio value (RMe). The estimated mixture ratio value is obtained by a model generating estimated mixture ratio values from at least one of the two signals for controlling control valves and/or the measured pressure.
IPC 8 full level
F02K 9/56 (2006.01); F02K 9/00 (2006.01); F02K 9/96 (2006.01)
CPC (source: EP US)
F02K 9/00 (2013.01 - EP US); F02K 9/56 (2013.01 - EP US); F02K 9/58 (2013.01 - US); F02K 9/96 (2013.01 - EP US); F05D 2270/709 (2013.01 - EP US)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
DOCDB simple family (publication)
WO 2017021651 A1 20170209; CN 108026864 A 20180511; EP 3332108 A1 20180613; EP 3332108 B1 20190529; FR 3039859 A1 20170210; FR 3039859 B1 20170901; JP 2018526564 A 20180913; RU 2018107852 A 20190906; US 2018258883 A1 20180913
DOCDB simple family (application)
FR 2016052011 W 20160802; CN 201680045746 A 20160802; EP 16757319 A 20160802; FR 1501683 A 20150806; JP 2018506114 A 20160802; RU 2018107852 A 20160802; US 201615750311 A 20160802